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时间:2011-04-01 19:17来源:蓝天飞行翻译 作者:航空
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23  BUSHING (HINGE 4)  ID  0.4380  0.4385  0.4411  0.0045
BUSHING (HINGE 4)  OD  0.4365  0.4370  0.4360  X 
24  BUSHING (HINGE 4)  ID  0.3125  0.3135  0.3149  0.0045  X 
BOLT (HINGE 4)  OD  0.3110  0.3120  0.3070

Rudder Wear Limits
Figure 601 (Sheet 4)

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 27-21-11
 ALL  ú ú 02 Page 605 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  INSTR REPAIR 
DIAMETER  DIM. WEAR PER-MITTED  CLEAR-ANCE DIA MAX 
MIN  MAX 
25  BUSHING (HINGE 5)  ID  0.4375  0.4395  0.4414  0.0045 X 
BUSHING (HINGE 5)  OD  0.4365  0.4370  0.4353  X 
26  BUSHING (HINGE 5)  ID  0.3125  0.3130  0.3149  0.0045 X 
BOLT (HINGE 5)  OD  0.3110  0.3120  0.3070 
27  BUSHING (HINGE 5)  ID  0.4380  0.4385  0.4411  0.0045
BUSHING (HINGE 5)  OD  0.4365  0.4370  0.4360  X 
28  BUSHING (HINGE 5)  ID  0.3125  0.3135  0.3149  0.0045 X 
BOLT (HINGE 5)  OD  0.3110  0.3120  0.3070 
29  BUSHING (HINGE 6)  ID  0.4375  0.4395  0.4414  0.0045 X 
BUSHING (HINGE 6)  OD  0.4365  0.4370  0.4353  X 
30  BUSHING (HINGE 6)  ID  0.3125  0.3130  0.3149  0.0045 X 
BOLT (HINGE 6)  OD  0.3110  0.3120  0.3070 
31  BUSHING (HINGE 6)  ID  0.4380  0.4385  0.4411  0.0045
BUSHING (HINGE 6)  OD  0.4365  0.4370  0.4360  X 
32  BUSHING (HINGE 6)  ID  0.3125  0.3135  0.3149  0.0045 X 
BOLT (HINGE 6)  OD  0.3110  0.3120  0.3070 
33  BUSHING (HINGE 7)  ID  0.3750  0.3790  0.3808  0.0060  X 
BUSHING (HINGE 7)  OD  0.3740  0.3745  0.3729  X 
34  BUSHING (HINGE 7)  ID  0.2500  0.2505  0.2525  0.0040 X 
BOLT (HINGE 7)  OD  0.2485  0.2495  0.2480 
35  BUSHING (HINGE 7)  ID  0.3755  0.3760  0.3784  0.0045
BUSHING (HINGE 7)  OD  0.3740  0.3745  0.3735  X 
36  BUSHING (HINGE 7)  ID  0.2500  0.2540  0.2560  0.0080 X 
BOLT (HINGE 7)  OD  0.2485  0.2495  0.2480


CHROME PLATE THICKNESS 0.0030 INCH THE SUM OF THE TWO IS NOT TO BE MORE THAN 0.0060 INCH
Rudder Wear Limits
Figure 601 (Sheet 5)

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 27-21-11
 ALL  ú ú 01 Page 606 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 RUDDER - REMOVAL/INSTALLATION
_____________________________
 1.  General_______
 A.  This procedure contains the removal task for a graphite or aluminum rudder and the installation task for an aluminum rudder.
 TASK 27-21-12-004-042
 2.  Remove the Graphite or Aluminum Rudder______________________________________
 A.  Special Tools and Equipment
 (1)  
F80025-1, Rudder Sling Assembly

 B.  
References

 (1)  
27-21-11/401, Rudder

 C.  
Access

 (1)  
Location Zones
 708 Rudder


 (2)  
Access Panels
 9512L TE Access Panel - Rudder
 9514R TE Access Panel - Rudder
 9515L TE Access Panel - Rudder


 D.  
Procedure


 S 024-001
 (1)  Remove the rudder and keep all the hardware for installation (Ref 27-21-11/401).
 
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